Method, based on elastic theory for plate buckling and results for 24S-T aluminum alloy Z-stiffened panels, is shown for calculating compressive strength of Z-stiffened panels that develop local instability.


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    Title :

    Method of calculating compressive strength of Z-stiffened panels that develop local instability


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English






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